01797nam 2200529 450 991070655400332120171129131529.0(CKB)5470000002456907(OCoLC)1013466540(EXLCZ)99547000000245690720171129j200104 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierHigh temperature fatigue crack growth behavior of Alloy 10 /John GaydaCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,April 2001.1 online resource (14 pages) illustrationsNASA/TM ;2001-210814"April 2001.""Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.Includes bibliographical references (page 4).Crack propagationnasatEngine designnasatFracture strengthnasatHeat of solutionnasatHigh strength alloysnasatNiobiumnasatTantalumnasatThermal fatiguenasatCrack propagation.Engine design.Fracture strength.Heat of solution.High strength alloys.Niobium.Tantalum.Thermal fatigue.Gayda John1400320NASA Glenn Research Center,GPOGPOBOOK9910706554003321High temperature fatigue crack growth behavior of Alloy 103476733UNINA